As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EVALUATION OF FUSELAGE NOSE REPAIR (AERODYNAMIC BODY FILLER) BETWEEN FRAMES 3 AND 4 CENTERLINE, JUST AFT OF LOWER EDGE OF RADOME. EVALUATED REPAIR, FOUND REPAIR NOT TO CONFORM TO FEDEX SRM. REMOVED DAMAGED AREA IAW 53-11-12 FIG 201. FABRICATED AND INSTALLED REPAIR IAW SRM 53-11-12 FIG 201. MATERIAL P/N A57210234200.